Aeroelastic and Dynamic Structural Analysis of a non-tapered wing
Auteur:
Alvaro Moral Aranda, Agustín Pérez Arjona, Vincenzo Rosciano, Alvaro Sanjuán Florido and Alfonso Velencoso Gómez.
Last Updated:
il y a 5 ans
License:
Creative Commons CC BY 4.0
Résumé:
In this document a thorough analysis of flutter will be presented, applied on a wing box which has been discretized using a FEM tool, MSC. NASTRAN, to cover both the dynamic structural analysis as well as the aeroelastic solution to flutter. Once the structural part has been detailed, a discussion about the flutter speed obtained with the Nastran SOL 145 will be presented, followed by some other solutions.
\begin
Discover why 18 million people worldwide trust Overleaf with their work.